FLOW COMPUTATION THROUGH THE PASSAGE BOUNDED BY THE DISH AND SUPPORTS OF THE AWACS
A numerical method has been introduced to predict the flow through a complex geometry bounded by the fuselage, airfoil supports and rotating dish of the AWACS. The finite volume computational approach is used to carry out all computations with staggered grid arrangement. The (k-ε) turbulence model...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
University of Baghdad
2007-03-01
|
| Schriftenreihe: | Journal of Engineering |
| Schlagworte: | |
| Online-Zugang: | https://joe.uobaghdad.edu.iq/index.php/main/article/view/2425 |
| Tags: |
Keine Tags, Fügen Sie das erste Tag hinzu!
|